Dynamic analysis of structural systems using component modes

Jet Propulsion Laboratory, California Institute of Technology

Under, each component is in a condition of dynamic equilibrium. Reactions at fixed constraints that may exist are not found by the foregoing calculations because these do no work on component displacements

10.1007/978-1-4899-5850-1

10.2514/8.3664

Turner M. J., 1964, Matrix Methods of Structural Analysis, edited by

Argyris J. H., 1963, Modern Fuselage Analysis and the Elastic Aircraft

10.2514/3.1483

Hurty W. C., 1960, J. Eng. Mech. Div, 86, 51, 10.1061/JMCEA3.0000162

Hurty W. C., 1964, Jet Propulsion Lab.

10.1016/0022-460X(64)90006-9